DE602006019960D1 - ARMED SUPPORT AND METHOD AND FIBER LAMINATE - Google Patents

ARMED SUPPORT AND METHOD AND FIBER LAMINATE

Info

Publication number
DE602006019960D1
DE602006019960D1 DE602006019960T DE602006019960T DE602006019960D1 DE 602006019960 D1 DE602006019960 D1 DE 602006019960D1 DE 602006019960 T DE602006019960 T DE 602006019960T DE 602006019960 T DE602006019960 T DE 602006019960T DE 602006019960 D1 DE602006019960 D1 DE 602006019960D1
Authority
DE
Germany
Prior art keywords
fiber laminate
armed support
armed
support
laminate
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
DE602006019960T
Other languages
German (de)
Inventor
Klaus Edelmann
Jens Bold
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Operations GmbH filed Critical Airbus Operations GmbH
Publication of DE602006019960D1 publication Critical patent/DE602006019960D1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06—Fibrous reinforcements only
    • B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
    • B29C70/205—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres the structure being shaped to form a three-dimensional configuration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/28—Shaping operations therefor
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0003—Producing profiled members, e.g. beams
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/065—Spars
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
DE602006019960T 2005-06-22 2006-06-20 ARMED SUPPORT AND METHOD AND FIBER LAMINATE Active DE602006019960D1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102005028765.4A DE102005028765B4 (en) 2005-06-22 2005-06-22 Method for producing a reinforcing profile
PCT/EP2006/063364 WO2006136560A1 (en) 2005-06-22 2006-06-20 Reinforcement beam as well as method and fiber laminate for manufacturing the reinforcement beam

Publications (1)

Publication Number Publication Date
DE602006019960D1 true DE602006019960D1 (en) 2011-03-17

Family

ID=36754711

Family Applications (2)

Application Number Title Priority Date Filing Date
DE102005028765.4A Expired - Fee Related DE102005028765B4 (en) 2005-06-22 2005-06-22 Method for producing a reinforcing profile
DE602006019960T Active DE602006019960D1 (en) 2005-06-22 2006-06-20 ARMED SUPPORT AND METHOD AND FIBER LAMINATE

Family Applications Before (1)

Application Number Title Priority Date Filing Date
DE102005028765.4A Expired - Fee Related DE102005028765B4 (en) 2005-06-22 2005-06-22 Method for producing a reinforcing profile

Country Status (9)

Country Link
US (2) US8105523B2 (en)
EP (1) EP1893478B1 (en)
JP (1) JP4977696B2 (en)
CN (1) CN101198518B (en)
BR (1) BRPI0611746A2 (en)
CA (1) CA2606988A1 (en)
DE (2) DE102005028765B4 (en)
RU (1) RU2424153C2 (en)
WO (1) WO2006136560A1 (en)

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US8632653B2 (en) 2005-05-03 2014-01-21 The Boeing Company Method of manufacturing curved composite structural elements
EP1884516A1 (en) 2006-08-04 2008-02-06 Ferrer Internacional, S.A. Pyrazolo[1,5-a]pyrimidines, processes, uses and compositions
US9511571B2 (en) 2007-01-23 2016-12-06 The Boeing Company Composite laminate having a damping interlayer and method of making the same
DE102007052672B4 (en) * 2007-11-05 2016-12-01 Airbus Operations Gmbh Fuselage structure of an aircraft for simplified laying and fixing of holders for attachment of lines
US9278484B2 (en) * 2008-04-17 2016-03-08 The Boeing Company Method and apparatus for producing contoured composite structures and structures produced thereby
US8349105B2 (en) * 2008-04-17 2013-01-08 The Boeing Company Curved composite frames and method of making the same
US8932423B2 (en) 2008-04-17 2015-01-13 The Boeing Company Method for producing contoured composite structures and structures produced thereby
US9090028B2 (en) 2008-04-17 2015-07-28 The Boeing Company Method for producing contoured composite structures and structures produced thereby
DE102008028865B4 (en) * 2008-06-19 2015-04-02 Airbus Defence and Space GmbH Process for the production of fiber composite profile components, as well as use of such manufactured fiber composite profile components
DE102008059653B4 (en) * 2008-11-28 2015-07-09 Gkn Aerospace Services Ltd. Flat component of an aircraft and method for its production
US8425710B2 (en) 2009-03-13 2013-04-23 The Boeing Company Automated placement of vibration damping materials
US8389424B2 (en) * 2009-11-11 2013-03-05 Albany Engineered Composites, Inc. Reinforcement for darted Pi preforms
DE102009047491A1 (en) * 2009-12-04 2011-06-09 Sgl Carbon Se Production of a 3D textile structure and semifinished fiber products from fiber composites
ES2383986B1 (en) 2009-12-30 2013-05-16 Airbus Operations, S.L. AIRCRAFT FUSELAGE NOTEBOOK IN COMPOSITE MATERIAL WITH STABILIZED SOUL.
ES2384349B1 (en) 2009-12-30 2013-05-16 Airbus Operations, S.L. AIRCRAFT FUSELAGE NOTEBOOK IN COMPOSITE MATERIAL WITH STABILIZING RIBS.
WO2012007780A1 (en) 2010-07-13 2012-01-19 Learjet Inc. Composite structure and method of forming same
US8652629B2 (en) * 2010-08-31 2014-02-18 Frp Transmission Innovations Inc. Transmission cross arm
JP5697506B2 (en) 2011-03-25 2015-04-08 シキボウ株式会社 Dry preform, annular structure made of composite material, and manufacturing method thereof
ES2645628T3 (en) 2011-12-01 2017-12-07 Airbus Operations S.L. Highly loaded frame of an aircraft fuselage with a lattice-shaped soul
US8771443B2 (en) * 2012-01-05 2014-07-08 The Boeing Company Method of fabricating a composite laminate enabling structural monitoring using electromagnetic radiation
US9404249B2 (en) * 2012-01-18 2016-08-02 Adc Acquisition Company Ultra light fiber placed truss
US9289949B2 (en) * 2012-06-08 2016-03-22 The Boeing Company Optimized cross-ply orientation in composite laminates
DE102012022713B3 (en) * 2012-11-21 2014-02-13 Diehl Aircabin Gmbh Panel and method of making a panel
EP2746018B1 (en) 2012-12-18 2017-03-01 Airbus Operations GmbH Method and apparatus for production of composite preform
US9290865B2 (en) * 2012-12-26 2016-03-22 Albany Engineered Composites, Inc. Three-dimensional woven corner fitting with lap joint preforms
RU2519301C1 (en) * 2013-02-18 2014-06-10 Иван Сергеевич Рыбкин Rib of alternating stiffness
DE102013223835A1 (en) * 2013-09-05 2015-03-05 Johnson Controls Components Gmbh & Co. Kg Composite component, in particular for a vehicle seat, and vehicle seat
RU2677169C1 (en) * 2013-12-14 2019-01-15 Зе Боинг Компани Bonded fibers in composite structures
US20160312863A1 (en) * 2013-12-16 2016-10-27 Borgwarner Inc. Composite tensioner arm or guide for timing drive application
JP5959558B2 (en) * 2014-03-13 2016-08-02 アイシン高丘株式会社 Composite structure and method for producing the same
DE102014222846A1 (en) * 2014-11-10 2016-05-12 Volkswagen Aktiengesellschaft Process for pultrusion Manufacture of fiber composite profile parts and fiber composite profile part
DE102015110195A1 (en) 2015-06-24 2016-12-29 Airbus Operations Gmbh Apparatus and method for forming a semi-finished fiber product
JP6581875B2 (en) * 2015-10-06 2019-09-25 三菱重工業株式会社 Composite material molding method
DE102016201366A1 (en) * 2016-01-29 2017-08-03 Volkswagen Aktiengesellschaft Fiber structure band and pultruded fiber composite profile
US10220935B2 (en) * 2016-09-13 2019-03-05 The Boeing Company Open-channel stiffener
RU171987U1 (en) * 2016-12-19 2017-06-23 Акционерное общество "Научно-исследовательский институт Приборостроения имени В.В. Тихомирова" Tooling for manufacturing antenna fairing elements
ES2958761T3 (en) * 2019-11-13 2024-02-14 Airbus Operations Slu Device and method of forming a composite laminate to obtain a Z-shaped profile
CN112173062A (en) * 2020-09-25 2021-01-05 中国直升机设计研究所 Composite material integrated frame beam and manufacturing method thereof
WO2022105976A1 (en) * 2020-11-19 2022-05-27 Vestas Wind Systems A/S Wind turbine blade shear web

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DE2622163C3 (en) * 1976-05-19 1983-05-26 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Profile support made of fiber-reinforced material
US4576849A (en) * 1983-06-06 1986-03-18 Hercules Incorporated Curved composite beam
DE3614618A1 (en) 1986-04-30 1987-11-05 Messerschmitt Boelkow Blohm SHELL STRUCTURE MADE OF FIBER REINFORCED PLASTIC
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GB9828368D0 (en) * 1998-12-22 1999-02-17 British Aerospace Forming reinforcing components
US6276105B1 (en) * 1999-01-11 2001-08-21 Henkel Corporation Laminate reinforced beam with tapered polymer layer
AU2002216657A1 (en) * 2000-11-15 2002-05-27 Toyota Motor Sales, U.S.A., Inc. One-piece closed-shape structure and method of forming same
EP1335821A1 (en) * 2000-11-21 2003-08-20 EADS Deutschland GmbH Technical production method, tension module and sewing material holder for creating textile preforms for the production of fibre-reinforced plastic components
DE10153875A1 (en) * 2001-11-02 2003-05-15 Bpw Bergische Achsen Kg Component in an elongated construction made of a fiber-plastic composite
US7384585B2 (en) * 2003-01-14 2008-06-10 Shikibo Ltd. Method for producing dry preform for composite material
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Also Published As

Publication number Publication date
JP4977696B2 (en) 2012-07-18
RU2424153C2 (en) 2011-07-20
RU2007144506A (en) 2009-07-27
EP1893478A1 (en) 2008-03-05
EP1893478B1 (en) 2011-02-02
WO2006136560A1 (en) 2006-12-28
JP2008543670A (en) 2008-12-04
US20090026315A1 (en) 2009-01-29
CN101198518B (en) 2012-02-29
US20120119030A1 (en) 2012-05-17
CN101198518A (en) 2008-06-11
US8105523B2 (en) 2012-01-31
CA2606988A1 (en) 2006-12-28
DE102005028765A1 (en) 2006-12-28
DE102005028765B4 (en) 2016-01-21
BRPI0611746A2 (en) 2010-09-28

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